Safety record in brief:1 NTSB accident (substantial damage, Mar 2003)3 ADs may apply
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Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
Loss of partial engine power for undetermined reasons during the initial climb after takeoff. Loose gravel/sandy was a factor during the landing roll.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA03LA049)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (172G) |
| 2011-06-02 | Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type… | May 26, 2011 | Airframe (172G)Only with: Modified by STC SA01303WI (installation of TAE 125-01 or TAE 125-02-99 engine). |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.